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Super Invar 32-5/4J32/K93500/Super Invar Tube Bar Rod Sheet
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Super Invar 32-5/4J32/K93500/Super Invar Tube Bar Rod Sheet
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Super Invar 32-5/4J32/K93500/Super Invar Tube Bar Rod Sheet
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Super Invar 32-5/4J32/K93500/Super Invar Tube Bar Rod Sheet
Super Invar 32-5/4J32/K93500/Super Invar Tube Bar Rod Sheet
Super Invar 32-5/4J32/K93500/Super Invar Tube Bar Rod Sheet

Super Invar 32-5/4J32/K93500/Super Invar Tube Bar Rod Sheet

  • Place of Origin Jiangsu,China
  • Model Number K93500
  • Trade Names Super Invar 32-5/ 4J32
  • Dimensions Customized Size
  • Delivery Conditions Grinding. Polished. Bright.
  • Avaliable Shapes Bar,Tube,Pipe,Wire,Foil,Strip,Ring,Fastener.Customized
  • MOQ 50~200 (KG)
  • Production Standards YB/T 5241-2014,ASTM F1684
  • Packaging Details Wooden Case, or as per Client's request
  • Payment Terms L/C, T/T, Western Union, MoneyGram
  • Trade Terms FOB, CIF, DUP, EXW
  • Delivery Time 7~40 days

Overview


4J32 alloy, also known as super-tile (Super-Invar) alloy. In the temperature range of -60 ~ 80 ℃, the expansion coefficient is lower than that of 4J36 alloy, but the stability of low temperature is worse than that of 4J36 alloy.

 

The alloy is mainly used in the manufacture of precision instrumentation parts requiring high dimensional dimensions within the range of ambient temperature changes. Alloy 1.5 according to the provisions of the heat treatment system, and then by -60 ℃ cold speed 2h, should not appear martensite. However, when the alloy composition is not properly, at different temperatures of the austenite (γ) to the needle-like martensite (α) at room temperature or low temperature, the phase change is accompanied by the volume expansion effect.

 

The expansion coefficient of the alloy increases accordingly. The main factors that affect the stability of the alloy at low temperature are the chemical composition of the alloy. It can be seen from the Fe-Ni-Co ternary phase diagram that nickel is the main element of the stable γ phase. The high nickel content favors the stability of the γ phase.

 

Copper is also an important element of stable alloying. With the total deformation rate of the alloy increases, the organization tends to be more stable. Segregation of alloy components may also cause γ → α phase transformation in local regions. In addition, grain thickness will also promote γ → α phase transition



Limiting Chemical Composition, %


Iron.............................................................................................................................................Balance.

Nickel....................................................................................................................................31.50-33.00

Cobalt.......................................................................................................................................3.20-4.20

Copper......................................................................................................................................0.40-0.80

Manganese.......................................................................................................................0.20-0.60 max.

Silicon........................................................................................................................................0.02 max.

Sulfur.........................................................................................................................................0.02 max.

Phosphorus................................................................................................................................0.02 max.

Carbon.......................................................................................................................................0.05 max.



Physical Constants


Density

lb/in^3............................................................0.292

g/cm^3.............................................................8.10

Melting Range

°F ..........................................................2606-2642

°C ..........................................................1430-1450

Curie Temperature

°C......................................................................220

Electrical Resistivity

µΩ•cm.............................................................0.77 

Thermal conductivity

W/(m·°C)..........................................................13.9




Mechanical properties


Alloy state

Tensile strength(σb/MPa)

Yield strength(σP0.2/MPa)

Elongation δ/%

Solid solution

≥470

≥302

≥44



Corrosion Resistance


The main components of 4J36 alloy include nickel, iron and a small amount of chromium. The nickel content is more than 35%, giving the alloy excellent corrosion resistance and oxidation resistance. The iron content is close to 64%, giving the alloy excellent magnetic properties and high strength. The chromium content is about 2%, so that the alloy has good heat resistance and wear resistance. In addition, although the content of carbon is very small, less than 0.1%, it also has an important impact on the mechanical properties and corrosion resistance of the alloy. This alloy has good corrosion resistance in dry air at room temperature, but in humid air or other harsh environments, the possibility of corrosion (rust) will increase.



Heat treatment


Solution treatment: At a temperature of about 850 to 900°C, the alloy is heated to full solution and then rapidly cooled. This treatment can improve the uniformity of the alloy, reduce the carbide precipitation at the grain boundary, and improve the stability of the thermal expansion coefficient of the alloy.


Cooling treatment: After solution treatment, the alloy is cooled rapidly to a low temperature, usually in liquid nitrogen. This treatment can further stabilize the thermal expansion coefficient of the alloy and reduce the change of thermal expansion.


In addition to the above two basic heat treatment methods, the heat treatment of 4J36 alloy also includes the following annealing treatment:

Stress relief annealing: mainly used to eliminate the residual stress of parts after machining. The treatment condition is held at 530 ~ 550℃ for 1 ~ 2 hours, and then the furnace is cooled.

Intermediate annealing: The purpose is to eliminate the alloy in the process of cold rolling, cold drawing, cold stamping caused by the work hardening phenomenon, in order to facilitate continued processing. The workpiece should be heated to 830 ~ 880℃, held for 30 minutes, furnace cooling or air cooling.


Stabilization treatment: In order to obtain a stable alloy with a low coefficient of expansion. This treatment usually consists of three stages: homogenization, tempering, and stabilizing aging.

In addition, 4J36 alloys cannot be hardened by heat treatment. During the heat treatment process, the change of alloy composition caused by welding should be avoided, so it is best to use argon arc welding, and the filler metal of welding is best to contain 0.5% to 1.5% titanium to reduce the porosity and cracks of welding.


In addition, 4J36 alloys cannot be hardened by heat treatment. During the heat treatment process, the change of alloy composition caused by welding should be avoided, so it is best to use argon arc welding, and the filler metal of welding is best to contain 0.5% to 1.5% titanium to reduce the porosity and cracks of welding.



Available Forms


We provide you with a variety of product forms, including but not limited to


● Bar & Rod

● Pipe &Tube

● Coil & Strip

● Plate & Sheet/Circle

● Wire & Welding

● Fitting (Flange, Bolts ,Elbow, Tee...)

● Customize

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